CN107214990B - A kind of daggers and swords formula method for winding of carbon fiber and carbon fiber bar processing technology based on this method - Google Patents
A kind of daggers and swords formula method for winding of carbon fiber and carbon fiber bar processing technology based on this method Download PDFInfo
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- CN107214990B CN107214990B CN201710606655.7A CN201710606655A CN107214990B CN 107214990 B CN107214990 B CN 107214990B CN 201710606655 A CN201710606655 A CN 201710606655A CN 107214990 B CN107214990 B CN 107214990B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0046—Producing rods
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- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01K—ANIMAL HUSBANDRY; CARE OF BIRDS, FISHES, INSECTS; FISHING; REARING OR BREEDING ANIMALS, NOT OTHERWISE PROVIDED FOR; NEW BREEDS OF ANIMALS
- A01K87/00—Fishing rods
Abstract
A kind of daggers and swords formula method for winding of carbon fiber and carbon fiber bar processing technology based on this method, daggers and swords formula method for winding includes the following steps: unidirectionally to wind, reinforces reverse-winding, lock section is fixed.A kind of carbon fiber bar processing technology includes the following steps: to prepare raw material line layer, coating polyacrylamide, overlay film vacuum processing, high pressure rolling fusion treatment, hot setting processing.Present invention line is instead of cloth, the intensity and hardness of carbon fiber itself can be given full play to, this kind of material arrangement mode can utmostly reinforce the synthesis stress-bearing capability of material, and it is not susceptible to be broken, in fishing rod use process, can be stable when comprehensive stress give reaction force, be the basis for the synthesis that fishing rod realizes itself power, daggers and swords formula coiled material mode is for hand handle section and No. 6 sections herein.
Description
Technical field:
Carbon fiber bar processing technology the present invention relates to a kind of daggers and swords formula method for winding of carbon fiber and based on this method.
Background technique:
Nowadays it is referred to as T-type commonly using the two kinds of carbon fibre material one kind for making high-end fishing rod in the market,
One kind being referred to as M type.Generally all 75% or so, resin content 25% or so has fine the phosphorus content of T-type carbon fibre material
Stretching and tough sexual function, defect causes the decline of its hardness, weight to lay particular stress on precisely due to content resin is excessively high.M type carbon fiber
Cloth phosphorus content 85% or so, resin 15% or so have good hardness, and weight is also light, but since resin content is inclined
Low, its toughness and drawing effect substantially reduces.In addition, carbon fiber surface is smooth, inertia is big, has chemically active functional group
It is few, cause the interface binding intensity between carbon fiber and matrix resin low, there are more defects at interface, often becomes composite material
Weak link.And typically now raw material line layer is arranged by the way of carbon cloth package, so that the thickness of material is larger, but
It is that service performance does not reach due level, there is no the plans of solution to this for the prior art.
Summary of the invention:
In order to compensate for the shortcomings of the prior art, the present invention provides a kind of daggers and swords formula method for winding of carbon fiber and it is based on being somebody's turn to do
The carbon fiber bar processing technology of method, it enhances comprehensive stress-bearing capability, and thickness further decreases, and surface roughness drops significantly
Low, interlaminar shear strength greatly improves, and solves problems of the prior art.
Used technical solution is the present invention to solve above-mentioned technical problem:
A kind of daggers and swords formula method for winding of carbon fiber, includes the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock section are fixed: each raw material coil that the end 1 of second raw material line passes through the second coil layer is laminated on relatively
It forms the channel formed on each raw material coil of First Line ring layer and forms lock nodel line, lock nodel line is located at First Line ring layer and second
Between coil layer, raw material line layer is obtained.
A kind of carbon fiber bar processing technology, includes the following steps:
S1, raw material line layer is prepared;
S2, coating polyacrylamide: polyacrylamide is coated in raw material line layer surface, obtains polyacrylamide amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer;
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material;
S5, hot setting processing: material temperature is heated to 135- by heating by the fine and close carbon fibre material that S4 is obtained
150 DEG C, final products are made in forming and hardening, demoulding cutting.
Preferably, in S1, the mass fraction of carbon fiber is 89-92 parts in the raw material line layer, the mass fraction of resin
It is 8-12 parts.
Preferably, in S2, the polyacrylamide amine layer with a thickness of 0.85-1.0mm.
Preferably, in S3, the ring two-body cracking polymerization technique includes the following steps:
S31, in vacuum film formation equipment, solid-state ring two-body 150-170 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 680-700 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
Preferably, in S4, the surface roughness of the densification carbon fibre material is R0.2-R2.4 μm.
Preferably, in S5, the surface roughness of the densification carbon fibre material is R0.05-R0.1 μm.
Preferably, in S5, heating method is electromagnetic heating.
Preferably, in S4, temperature is controlled at 90-110 DEG C, and rolling drafts is 0.08-0.12mm.
The present invention using the above scheme, with line instead of cloth, can give full play to the intensity and hardness of carbon fiber itself, this kind
Material arrangement mode can utmostly reinforce the synthesis stress-bearing capability of material, and be not susceptible to be broken, in fishing rod use process
In, it is the basis for the synthesis that fishing rod realizes itself power that when comprehensive stress can be stable, which gives reaction force, herein daggers and swords formula
Coiled material mode is for hand handle section and No. 6 sections;In addition to this, carbon fiber surface surface roughness can be increased to from original Ra6.3
Ra2.4~Ra0.2 can be realized the mirror surface accuracy of Ra0.05-0.1 by control condition;And surface is made to obtain squeezing hardening, it is resistance to
Mill property, fatigue strength improve;Surface stress plastic deformation is eliminated, dimensional accuracy can relatively long-term holding stabilization;By rolling
Afterwards, Carbon fibers Carbon fibers hardness can be improved 15~30%, and fatigue resistance improves 15% or more;Due to rolled fiber carbon fiber
Surface deformation is tieed up, textura epidermoidea's cold hardening and crystal grains fine are made, forms fine and close threadiness, and form residual stress layer, hardness
It is improved with intensity, so as to improve the wearability, corrosion resistance and conformability on original carbon fiber surface, high pressure rolls fusion treatment technology
The interlaminar shear strength of final products is set to be increased to 100MPa or so by 55-70MPa.
Detailed description of the invention:
Fig. 1 is method for winding schematic diagram of the invention.
Specific embodiment:
In order to clarify the technical characteristics of the invention, below by specific embodiment, and its attached drawing is combined, to this hair
It is bright to be described in detail.
As shown in Figure 1, a kind of daggers and swords formula method for winding of carbon fiber, includes the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
A kind of carbon fiber bar processing technology, includes the following steps:
S1, raw material line layer is prepared;
S2, coating polyacrylamide: polyacrylamide is coated in raw material line layer surface, obtains polyacrylamide amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer;
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material;
S5, hot setting processing: material temperature is heated to 135- by heating by the fine and close carbon fibre material that S4 is obtained
150 DEG C, final products are made in forming and hardening, demoulding cutting.
In S1, the mass fraction of carbon fiber is 89-92 parts in the carbon cloth, and the mass fraction of resin is 8-11
Part.The content for improving carbon itself can be improved the hardness of material and mitigate weight.
In S2, the polyacrylamide amine layer with a thickness of 0.85-1.0mm.As the transition zone outside raw material line layer, by
There is caking property in itself, so it is two layers inside and outside to can be good at fusion, and can make up for it raw material line layer carbon content height and make
At toughness weaken the shortcomings that, improve the toughness of its own.
In S3, the ring two-body cracking polymerization technique includes the following steps:
S31, in vacuum film formation equipment, solid-state ring two-body 150-170 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 680-700 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
In S4, the surface roughness of the densification carbon fibre material is R0.2-R2.4 μm.
In S5, the surface roughness of the densification carbon fibre material is R0.05-R0.1 μm.Since high pressure rolling is handled
Carbon fibre material is routine techniques, can control its surface roughness by control high pressure roll unit, due to polyacrylamide
The addition of layer, thus surface roughness can further decrease, to improve the feel of user.
In S5, heating method is electromagnetic heating.Electromagnetic heating is interior heating method, suitable for fine and close carbon fibre material
Hot setting processing.
Embodiment 1:
S1, production raw material line layer;The mass fraction of carbon fiber is 89 parts in the carbon fiber, and the mass fraction of resin is 11
Part, specifically comprise the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
S2, coating polyacrylamide: in the polyacrylamide of raw material line layer surface coating 0.85mm thickness, polyacrylamide is obtained
Amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 150 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 680 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material, at 90 DEG C, rolling drafts is 0.08mm for temperature control;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
135 DEG C, No. 1 product is made in forming and hardening.
Embodiment 2:
S1, production raw material line layer;The mass fraction of carbon fiber is 92 parts in the carbon fiber, and the mass fraction of resin is 8
Part, specifically comprise the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
S2, coating polyacrylamide: in the polyacrylamide of raw material line layer surface coating 1.0mm thickness, polyacrylamide is obtained
Amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 170 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 700 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material, at 110 DEG C, rolling drafts is 0.12mm for temperature control;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
150 DEG C, No. 2 products are made in forming and hardening.
Embodiment 3:
S1, production raw material line layer;The mass fraction of carbon fiber is 90.5 parts in the carbon cloth, the mass fraction of resin
It is 9.5 parts, specifically comprises the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
S2, coating polyacrylamide: in the polyacrylamide of raw material line layer surface coating 0.93mm thickness, polyacrylamide is obtained
Amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 160 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 690 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material, at 100 DEG C, rolling drafts is 0.1mm for temperature control;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
143 DEG C, No. 3 products are made in forming and hardening.
Embodiment 4:
S1, production raw material line layer;The mass fraction of carbon fiber is 89 parts in the carbon fiber, and the mass fraction of resin is 11
Part, specifically comprise the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
S2, it is not coated by polyacrylamide, directly progress S3;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 150 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 680 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material, at 90 DEG C, rolling drafts is 0.08mm for temperature control;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
135 DEG C, No. 4 products are made in forming and hardening.
Embodiment 5:
S1, production raw material line layer;The mass fraction of carbon fiber is 92 parts in the carbon cloth, and the mass fraction of resin is
8 parts, specifically comprise the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
S2, it is not coated by polyacrylamide, directly progress S3;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 170 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 700 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material, at 110 DEG C, rolling drafts is 0.12mm for temperature control;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
150 DEG C, No. 5 products are made in forming and hardening.
Embodiment 6:
S1, production raw material line layer;The mass fraction of carbon fiber is 90.5 parts in the carbon cloth, the mass fraction of resin
It is 9.5 parts, specifically comprises the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
S2, it is not coated by polyacrylamide, directly progress S3;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 160 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 690 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material, at 100 DEG C, rolling drafts is 0.1mm for temperature control;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
143 DEG C, No. 6 products are made in forming and hardening.
Embodiment 7:
S1, production raw material line layer;The mass fraction of carbon fiber is 89 parts in the carbon cloth, and the mass fraction of resin is
11 parts, specifically comprise the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
S2, coating polyacrylamide: in the polyacrylamide of raw material line layer surface coating 0.85mm thickness, polyacrylamide is obtained
Amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 150 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 680 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, fusion treatment is rolled without high pressure, is directly entered S5;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
135 DEG C, No. 7 products are made in forming and hardening.
Embodiment 8:
S1, production raw material line layer;The mass fraction of carbon fiber is 92 parts in the carbon cloth, and the mass fraction of resin is
8 parts, specifically comprise the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
S2, coating polyacrylamide: in the polyacrylamide of raw material line layer surface coating 1.0mm thickness, polyacrylamide is obtained
Amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 170 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 700 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, fusion treatment is rolled without high pressure, is directly entered S5;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
150 DEG C, No. 8 products are made in forming and hardening.
Embodiment 9:
S1, production raw material line layer;The mass fraction of carbon fiber is 90.5 parts in the carbon cloth, the mass fraction of resin
It is 9.5 parts, specifically comprises the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, and the end 2 of raw material line is fixed,
End 1 reaches requirement length around the winding of model bar, and the first coil being made of several spiral shape raw material coils is formed on model bar
Layer;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, end 1 reaches requirement around the winding of model bar
Length forms the second coil layer being made of several spiral shape raw material coils, each raw material coil point of the second coil layer of composition
Not opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms First Line ring layer
Each raw material coil on the channel that is formed form lock nodel line, lock nodel line is located between First Line ring layer and the second coil layer, obtains
To raw material line layer.
S2, coating polyacrylamide: in the polyacrylamide of raw material line layer surface coating 0.93mm thickness, polyacrylamide is obtained
Amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 160 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 690 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, fusion treatment is rolled without high pressure, is directly entered S5;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
143 DEG C, No. 9 products are made in forming and hardening.
Embodiment 10:
S1, production raw material line layer is wound using carbon cloth.
S2, coating polyacrylamide: in the polyacrylamide of raw material line layer surface coating 0.85mm thickness, polyacrylamide is obtained
Amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 150 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 680 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material, at 90 DEG C, rolling drafts is 0.08mm for temperature control;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
135 DEG C, No. 10 products are made in forming and hardening.
Embodiment 11:
S1, production raw material line layer is wound using carbon cloth.
S2, coating polyacrylamide: in the polyacrylamide of raw material line layer surface coating 1.0mm thickness, polyacrylamide is obtained
Amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 170 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 700 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material, at 110 DEG C, rolling drafts is 0.12mm for temperature control;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
150 DEG C, No. 11 products are made in forming and hardening.
Embodiment 12:
S1, production raw material line layer is wound using carbon cloth.
S2, coating polyacrylamide: in the polyacrylamide of raw material line layer surface coating 0.93mm thickness, polyacrylamide is obtained
Amine layer;
S3, overlay film are vacuum-treated: being cracked polymerization technique by ring two-body and polymerize to form poly- pair in the material surface that S2 is obtained
Diformazan benzene layer, steps are as follows:
S31, in vacuum film formation equipment, solid-state ring two-body 160 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 690 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear poly- pair
Dimethylbenzene film.
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains densification
Carbon fibre material, at 100 DEG C, rolling drafts is 0.1mm for temperature control;
S5, hot setting processing: material temperature is heated to by the fine and close carbon fibre material that S4 is obtained by electromagnetic heating
143 DEG C, No. 12 products are made in forming and hardening.
Surface roughness, interlaminar shear strength and the material thickness for measuring 1-9 product, obtain following table
It can be seen that from above-mentioned test result and obtain raw material line layer by the way of winding, intensity can not influenced
Under the premise of fishing rod thickness is greatly reduced, pass through be added polyacrylamide amine layer, it will be apparent that improve interlaminar shear strength, reduce
Roughness after rolling;And high pressure rolling is utilized to handle, while significantly improving interlaminar shear strength, also significantly
Reduce roughness.
Above-mentioned specific embodiment cannot function as limiting the scope of the invention, for the technology people of the art
For member, any alternate modification or transformation made to embodiment of the present invention are fallen within the scope of protection of the present invention.
Place is not described in detail by the present invention, is the well-known technique of those skilled in the art of the present technique.
Claims (9)
1. a kind of daggers and swords formula method for winding of carbon fiber, characterized by the following steps:
S01, carbon fiber line is taken or that carbon cloth is cut into carbon fiber rope is spare as raw material line;
S02, unidirectional winding: taking selected model bar, and the raw material line is divided into end 1 and end 2, the end 2 of raw material line is fixed, end 1
Reach requirement length around the winding of model bar, forms the First Line ring layer being made of several spiral shape raw material coils on model bar;
S03, it reinforces reverse-winding: taking second raw material line, on the basis of S02, to reach requirement long around the winding of model bar at end 1
Degree forms the second coil layer being made of several spiral shape raw material coils, each raw material coil difference of the second coil layer of composition
Opposite is laminated on each raw material coil of composition First Line ring layer;
S04, lock, which save, to be fixed: opposite be laminated on of each raw material coil that end 1 passes through the second coil layer forms each of First Line ring layer
The channel formed on a raw material coil forms lock nodel line, and lock nodel line is located between First Line ring layer and the second coil layer, obtains original
Stockline layer.
2. a kind of carbon fiber bar processing technology of the raw material line layer using claim 1, it is characterised in that: including as follows
Step:
S1, raw material line layer is prepared;
S2, coating polyacrylamide: polyacrylamide is coated in raw material line layer surface, obtains polyacrylamide amine layer;
S3, overlay film are vacuum-treated: being polymerize to be formed in the material surface that S2 is obtained by ring two-body cracking polymerization technique and be gathered to diformazan
Benzene layer;
S4, high pressure roll fusion treatment: using high pressure roll unit, the material obtained with roller rolling press S3 obtains fine and close carbon fiber
Tie up material;
S5, hot setting processing: material temperature is heated to 135-150 by heating by the fine and close carbon fibre material that S4 is obtained
DEG C, final products are made in forming and hardening, demoulding cutting.
3. a kind of carbon fiber bar processing technology according to claim 2, it is characterised in that: in S1, the raw material line layer
The mass fraction of middle carbon fiber is 89-92 parts, and the mass fraction of resin is 8-12 parts.
4. a kind of carbon fiber bar processing technology according to claim 2, it is characterised in that: in S2, the polyacrylamide
Amine layer with a thickness of 0.85-1.0mm.
5. a kind of carbon fiber bar processing technology according to claim 2, it is characterised in that: in S3, the ring two-body is split
The technique that depolymerizes includes the following steps:
S31, in vacuum film formation equipment, solid-state ring two-body 150-170 DEG C distillation be gaseous state ring two-body;
S32, gaseous state ring two-body are cracked into stable unimolecule at 680-700 DEG C;
S33, unimolecule enter in vacuum deposition room, are adsorbed on the surface of S2 resulting materials, and polymerize and to form linear gather to diformazan
Benzene film.
6. a kind of carbon fiber bar processing technology according to claim 2, it is characterised in that: in S4, the densification carbon fiber
The surface roughness for tieing up material is R0.2-R2.4 μm.
7. a kind of carbon fiber bar processing technology according to claim 2, it is characterised in that: in S5, the densification carbon fiber
The surface roughness for tieing up material is R0.05-R0.1 μm.
8. a kind of carbon fiber bar processing technology according to claim 2, it is characterised in that: in S5, heating method is electricity
Magnetic heating.
9. a kind of carbon fiber bar processing technology according to claim 2, it is characterised in that: in S4, temperature is controlled in 90-
110 DEG C, rolling drafts is 0.08-0.12mm.
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19502038A1 (en) * | 1994-01-12 | 1995-07-13 | Wonder Co Ltd | Tubular fishing rod |
CN101142853A (en) * | 2005-03-17 | 2008-03-12 | 高盛股份有限公司 | Method for manufacturing pipe-type woven carbon fibers and carbon fiber heating lamp using the pipe-type woven carbon fibers |
CN101338854A (en) * | 2007-07-03 | 2009-01-07 | 天津甘泉集团有限公司 | Pulling and winding rod |
CN104044276A (en) * | 2014-06-29 | 2014-09-17 | 柳州美纳机械有限公司 | Manufacturing method for glass steel tube |
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Publication number | Priority date | Publication date | Assignee | Title |
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US8373657B2 (en) * | 2008-08-15 | 2013-02-12 | Qualcomm Incorporated | Enhanced multi-touch detection |
-
2017
- 2017-07-24 CN CN201710606655.7A patent/CN107214990B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19502038A1 (en) * | 1994-01-12 | 1995-07-13 | Wonder Co Ltd | Tubular fishing rod |
CN101142853A (en) * | 2005-03-17 | 2008-03-12 | 高盛股份有限公司 | Method for manufacturing pipe-type woven carbon fibers and carbon fiber heating lamp using the pipe-type woven carbon fibers |
CN101338854A (en) * | 2007-07-03 | 2009-01-07 | 天津甘泉集团有限公司 | Pulling and winding rod |
CN104044276A (en) * | 2014-06-29 | 2014-09-17 | 柳州美纳机械有限公司 | Manufacturing method for glass steel tube |
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